N828BX, cancelled May 1, 2014

Service difficulty reports · 147

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N828BX' AND deregistration_id = 'N828BX-2014-05-01'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IXXA110003SSkin · crackedDURING SKIN INSP FOR AD 2008-26-07, FOUND A .5 INCH CRACK ON LT WING LOWER SKIN AT STRINGER 58. MX PERFORMED INSP FOR FERRY FLIGHT FOR PERMANENT STORAGE IAW GMM 3.117.Jan 14, 2011 · N828BX · Doug DC871F · Wing, Plate/SkinSDR IXXA100015OPlug · unsecureDURING CRUISE, THE CREW SHUTDOWN NR 1 ENG DUE TO LOSS OF OIL QUANTITY. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND THE STARTER FILLER PLUG OFF. THEY REINSTALLED FILLER PLUG AND LOCKED SERVICED ENGINE. OPS CHECK GOOD IAW AMM 80-10, AMM 12-10. Feb 16, 2010 · N828BX · Doug DC871F · Turbine Engine Oil SystemSDR IXXA090042OFuel Control · out of rigDURING TAKEOFF, NR 4 ENG WOULD NOT MAKE PWR. ONCE AIRBORNE HAD TO PUSH THROTTLE PAST OTHER THROTTLES NR 4 EGT WENT TO 907 DEGREE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NR 4 ENG AND FOUND VSV'S AND VBV OUT OF RIG. MX ACCOMPLISAug 27, 2009 · N828BX · Doug DC871F · Fuel Controlling SystemSDR IXXA090041STee Fitting · crackedDURING INSP IAW AD2007-21-18 AND SB DC8-53A081 FOUND RT AFT PRESSURE BULKHEAD TEE FITTING CRACKED. STOP DRILLED CRACK IAW SRM 53-2-5.Aug 24, 2009 · N828BX · Doug DC871F · Fuselage Main, BulkheadSDR IXXA080035OConnector · defectiveDURING CRUISE FROM KTOL NUMBER THREE ENGINE OIL PRESSURE STABILIZED AT 50 PSI THEN FLUCTUATED BETWEEN 20-60 PSI FOR A SHORT TIME, THEN STABILIZED AGAIN AT 50 PSI. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OIL PRESSURDec 8, 2008 · N828BX · Doug DC871F · Engine Oil System WiringSDR IXXA080028OWire · brokenDURING TAKEOFF FROM KTOL F/O'S FLIGHT DIRECTOR FLAG IN ADI AND GYRO FLAG CAME IN VIEW. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINTENANCE SMART BOX WIRE NUMBER 2TN49B22 BROKEN AT R50-972 PIN 35. MAINTENANCE REPAIRED WIRE 2TN49B22. OPERATIONAL CHOct 21, 2008 · N828BX · Doug DC871F · Navigation System WiringSDR IXXA080027OComparator · defectiveDURING CLIMBOUT FROM KTOL, CAPT'S RMI, GYRO FLAG, AND F/O'S GLIDESLOPE IN HSI, FLIGHT DIRECTOR IN ASI FLAG ALL IN VIEW. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SMART BOX. OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCEOct 21, 2008 · N828BX · Doug DC871F · Integrated Flight SystemSDR IXX2008F00094Connector · damagedDURING CRUISE, NR (2) FIRE WARNING LIGHT CAME ON STEADY, THE CREW SHUTDOWN NR (2) ENGINE AND DISCHARGED (1) FIRE BOTTLE, LIGHT WENT OUT. (20 MINUTES OUT, NR (2) FIRE WARNING LIGHT CAME BACK ON MOMENTARILY AND FIRE LOOPS WOULD ONLY TEST INTERMITTENTLY, THE CRSep 6, 2008 · N828BX · Doug DC871F · Fire Protection System WiringSDR IXX2008F00022Fire Detector · false activationFLT ATN 819/KDFW TO KTOL/TAT 87593/TAC 36428. DURING CLIMBOUT FROM KDFW NR 4 FIRE WARNING LIGHT CAME ON, THE CREW SHUTDOWN NR 4 ENGINE AND DISCHARGED BOTH FIRE BOTTLES THE LIGHT REMAINED ON. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. MAINTENANCEJul 16, 2008 · N828BX · Doug DC871F · Fire DetectionSDR DHL2008F00016Fire Warning · activatedFLT NR ATN 819 / KDFW TO KTOL. DURING CLIMBOUT FROM KDFW NR 4 ENGINE FIRE WARNING LIGHT CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND LIGHT REMAINED ON. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WORK. (A)Jul 16, 2008 · N828BX · Doug DC871F · Fire DetectionSDR IXXA080006OFire Loop · looseDURING CRUISE FROM KPHL TO KTOL, NUMBER FOUR ENGINE SHORT LIGHT CAME ON WITH NO FIRE TEST INDICATION, THE CREW ACCOMPLISHED EMERGENCY PROCEDURES AND SHUT DOWN NUMBER FOUR ENGINE. THE CREW LANDED AT KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHTFeb 19, 2008 · N828BX · Doug DC871F · Fire DetectionSDR IXXA070051OFire Loop · false activationDURING CRUISE FROM KTOL TO KMCI, NR 4 ENGINE WAS SHUT DOWN FOR A SHORT CIRCUIT LIGHT ON WITH NO FIRE LIGHT OR ALARM BELL DURING TEST. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER 4 FIRE LOOPS, NO DEFECTS NOTED. OPERATIONAL CHECK WAS GOOD. Oct 5, 2007 · N828BX · Doug DC871F · Fire DetectionSDR IXXA070050ORelay · failedTHIRTY MINUTES AFTER TAKEOFF FROM KTOL NR 4 FIRE WARNING LIGHT CAME ON, THE CREW DISCHARGED BOTH NR 4 ENGINE FIRE BOTTLES INTO ENGINE, THE FIRE WARNING LIGHT WENT OUT AFTER THE SECOND BOTTLE WAS DISCHARGED. 5 MINUTES LATER FIRE WARNING WAS INTERMITTENT, NR 4 Oct 3, 2007 · N828BX · Doug DC871F · Fire DetectionSDR IXXA070049OFire Loop · defectiveDURING CLIMB-OUT FROM KTOL, THE CREW NOTICED NUMBER 4 FIRE WARNING LIGHT WAS INTERMITTENT. THE CREW RETURNED TO KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER FOUR FIRE WARNING SYSTEM AND REPLACED LEFT AFT FIRE LOOP, OPERATIONAL CHECK WAS GOOD IAW DC8 MOct 2, 2007 · N828BX · Doug DC871F · Fire DetectionSDR IXXA07SMN153SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 27 LEFT AT STATION 1699. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN154SFloorbeam · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOORBEAM WEB CORRODED AT STATION 960.000 RT BOTTOM LINE 40". REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED CORROSION. FOUND OUT OF LIMIT. FABRICATE REPAIR ANGLES OF EXTRUSION. CLEANEApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Floor BeamSDR IXXA07SMN155SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD SLOT VANE FITTING WITH CORROSION AT STATION XILD 0.7095. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. FABRICATED NEW FITTING. CLEANED, TREATED AND PRIMED AREA AND FITTING. APApr 21, 2007 · N828BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA07SMN156SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28RIGHT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN143SDoubler · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL FUSELAGE NOSE SECTION RIGHT AFT PRIMARY HEAT INTERCHANGER AFT LOWER CORNER DOUBLER CRACKED AT STATION -12 LONGERON 27 RIGHT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED TREATED AND PRIMED AREApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN142SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT FS 1725 LONGERON 16.5 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN138SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR INSTALLED AT A-PIT BASKET DOOR, RIGHT FORWARD JAMB CORNER AT STATION 293 LONGERON 30 RIGHT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER, TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN137SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR INSTALLED AT A-PIT BASKET DOOR, RIGHT AFT JAMB CORNER AT STATION 327 LONGERON 30 RIGHT. REMOVED EXISTING REPAIR. FABRICATED DOUBLER, TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIEDApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN140SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, IMPROPER REPAIR LOCATED AT STATION 1581 LONGERON 23 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. CApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN139SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 445, LONGERON 27.5 RIGHT. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, EXTERNAL DOUBLER AND INTERNAL DOUBLER, CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SUApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA070029SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 RIGHT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN,Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN135SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT AFT FUSELAGE SKIN PANEL AND SKIN SPLICES OF LONGERON 28 LEFT AT STATION 1690. REMOVED EXISTING EXTERNAL REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, Apr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN141SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION 1.600 LONGERON 28 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLER, INTERNAL DOUBApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN146SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP CRACKED ON UPPER PART EXTERNAL COATING AT STATION XW 104.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANTApr 21, 2007 · N828BX · Doug DC871F · Wing, Plate/SkinSDR IXXA07SMN150SFrame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME FLANGE WITH A CRACK AT STATION 1580.000 LONGERON 21LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT. PERFORMED HEAT TREATMApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, FrameSDR IXXA07SMN158SFrame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FRAME WITH A CRACK AT STATION 1260.000 LONGERON 34 RIGHT TO LONGERON 35 LEFT. REMOVED CRACKED FITTING. FABRICATED FRAME FITTING, SPLICES, AND DOUBLER. PERFORMED HEAT TREATMENT. PERFORMED NDT INApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, FrameSDR IXXA07SMN144SHook · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE AT NOSE SECTION FORWARD PAX DOOR HOLD OPEN HOOK, WAS CRACKED AT STATION 15.000 LONGERON 16 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT INApr 21, 2007 · N828BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA07SMN136SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL JOINT FITTING WITH CORROSION AT STATION 940.000 LONGERON 24 RIGHT. REMOVED CORROSION. FOUNDED OUT OF LIMITS REMOVED CORRODED FITTING. FABRICATED FRAME FITTING, SPLICES AND DOUBLER. Apr 21, 2007 · N828BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR IXXA07SMN145SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BATH TUB FITTING CORRODED, BETWEEN STATION 70.000 AND STATION 80.000 LONGERON 35 RIGHT. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN147SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR. UPPER SKIN DENT WITH CRACK AT STATION XE 156.468 AND STATION XE 161.375. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL REPAIR PARTS. BONDED PARTApr 21, 2007 · N828BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA07SMN148SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 RIGHT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 PAGE 22 FIGUREApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN149SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SECTION LONGERON 17 LEFT HAND, WITH A CRACK AT STATION 1766.000 TO STATION 1794.000. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LONGERON IAW DC8 SRM 53-5-1 PAGE 22 FIGUREApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA07SMN152SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAD CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL WELL CEILING BETWEEN STATION 960.000 - 980.000 LEFT BOTTOM LINE 40”. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN151SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, IN MAIN CARGO COMPARTMENT, FOUND CORROSION ON FITTING ABOVE MAIN LANDING GEAR WHEEL WELL CEILING BETWEEN STATION 960.000 - 980.000 RIGHT BOTTOM LINE 40". REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CApr 21, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN157SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN HAD A NON STANDARD REPAIR AT STATION XFS 426.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER NDT TEST. Apr 21, 2007 · N828BX · Doug DC871F · Wing, Plate/SkinSDR IXXA07SMN159SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON33 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED TREATED AND PRIMEDApr 11, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA07SMN160SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO BILGE INTERIOR FITTING CRACKED AT STATION 1260.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING PERFORMED NDT. NO CRACK OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPApr 11, 2007 · N828BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA060609OOil Filter · dirtyDURING CRUISE FROM KTOL TO KSJC, NUMBER 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ALL OTHER PARAMETERS WERE NORMAL. THE CREW SHUTDOWN THE ENGINE AND CONTINUED TO KSJC WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THNov 8, 2006 · N828BX · Doug DC871F · Turbine Engine Oil SystemSDR IXXA060172OFire Detector · shortedAT CRUISE FL 36.0 NR 3 ENGINE SHORT CIRCUIT LIGHT BEGAN FLASHING. FIRE WARNING WOULD NOT TEST, ENGINE SHUTDOWN PER COM PROCEDURE. THE CREW ELECTED TO RETURN THE AIRCRAFT TO TOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CONNECTOR FROM FORWARD SIDE OF Mar 9, 2006 · N828BX · Doug DC871F · Fire DetectionSDR IXXA060171OConnector · corrodedDURING FLIGHT 834 FROM TOL TO SJC APROX 50 MIN INTO FLIGHT, NR 3 ENG SHORT CIRCUIT AMBER LIGHT CAME ON. PERFORMED ABNORMAL CHECK LIST. THE LIGHT DID NOT EXTINGUISH, NOR DID THE FIRE WARNING TEST. PERFORMED ENGINE SHUTDOWN OTHER THAN FIRE DAMAGE. THE CREW EFeb 28, 2006 · N828BX · Doug DC871F · Fire Protection System WiringSDR IXXA0600037OSensing Element · defectiveON FLIGHT ATN833 FROM KSJC TO KRFD, NR 3 ENGINE FIRE WARNING LIGHT AND BELL CAME ON DESCENT TO KRFD. COMPLY WITH COMPANY PROCEDURES WIND MILLING TIME 30 MINUTES AND OIL PRESSURE WAS 20 PSI. CREW ELECTED TO LAND AT KTOL AND LANDED WITHOUT INCIDENT. MAINTENANJan 17, 2006 · N828BX · Doug DC871F · Fire DetectionSDR IXXA0500215ORadio · malfunctionedON FLIGHT 362 FROM KTOL TO KEWR NR 1 HF CONTINOUSLY ATTEMPTED TO TUNE ON ALL FREQUENCES WITH THE SAME RESULTS. THEN HF RADIO NR 2 WAS KEYED TO TUNE, THE AUTOPILOT KICKED OFF CAUSING THE AIRCRAFT TO YAW AND PITCH. DUE TO INTENDED FLIGHT PLAN, CREW ELECTED TO Dec 27, 2005 · N828BX · Doug DC871F · HF Communications SystemSDR IXXA0500118OBulb · looseDURING A TAKEOFF ROLLOUT AT 110KTS, NR 3 ENGINE OIL PRESSURE LIGHT CAME ON. TAKEOFF WAS REJECTED. OIL PRESSURE AND QUANTITY INDICATED NORMAL BUT LIGHT REMAINED ON UNTIL THE ENGINE WAS SHUTDOWN. CREW RETURNED TO BLOCKS. MAINTENANCE DEFERRED THIS IAW MEL 79-6 (CNov 22, 2005 · N828BX · Doug DC871F · Engine Indicating SystemSDR IXXA0500104OBlade · leakingNR 2 ENG SHUTDOWN FOR LOSS OF OIL QTY. OIL PRESS DROPPED. OIL TEMP STABLE. SHUTDOWN NR 2 ENG. WINDMILL OIL PRESS DROPPED & QTY INCREASED. TEMP STABLE. NO WINDMILLING PRESS. LOW PRESS LIGHT ILLUM. LANDED W/OUT INCIDENT. R&R NR 2 ENG, OPS & LEAK CHK GOOD. ACFT Aug 23, 2005 · N828BX · Doug DC871F · Turbine Engine Oil SystemSDR IXXA0500103OEngine · malfunctionedDURING CRUISE FROM KPHL TO KTOL THE NR 2 ENGINE FLUCTUATED EGT FOLLOWED BY A INSTANTANEOUS EGT TEMPERATURE INCREASE. OIL PRESSURE FLUCTUATED BUT NO LOSS. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN THEN LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS Aug 19, 2005 · N828BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA0500097OTube · broken!DURING CLIMBOUT FROM KTOL TO KPHL THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. PRESSURE WAS AT 14 PSI AND FLUCTUATING AND OIL QUANTITY DEPLETING SLOWLY. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. CREW LANDED IN KPHL WITHOUT INCIDENT. MAINTENAAug 18, 2005 · N828BX · Doug DC871F · Engine Oil System (Airframe Furnished)
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